Aerospace Engineering Lectures - Compressible Flow, Aerospace Engineering Lecture 12

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Summary

Keywords

Compressible aerodynamics Machmeter Aircraft Engineering Fluid Dynamics High Speed Flow How to measure aircraft velocity? compressible flow fluid mechanics aerodynamics isentropic relations isentropic relations aerodynamics principles of flight

Full Transcript

Static and total pressure, temperature and density for high speed compressible flow are explained. The isentropic relations are used to derive an equation to calculate the Mach number of an aircraft in flight from static and total pressure measurements. The true, calibrated and equivalent airspeed concepts are also defined. #aerospaceengineering #gateaerospaceengineering #aerodynamics #fluidmechanics

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